FIELD: engines and pumps.
SUBSTANCE: proposed compressor comprises first component 23 and first sliding component 24. The former can be subjected to laser welding. Said first sliding component 24 consists of cast iron that can be subjected laser welding and features carbon content varying from 2.0 wt % or more to 2.7 wt % or less. Said first sliding component 24 is jointed to the first component 23 by laser welding without butt interlayer.
EFFECT: reduced sizes, lower costs.
19 cl, 25 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMPRESSOR MANUFACTURING METHOD AND COMPRESSOR | 2007 |
|
RU2403449C2 |
| COMBUSTION CHAMBER AND GAS TURBINE ENGINE COMPRISING SUCH COMBUSTION CHAMBER | 2019 |
|
RU2738248C1 |
| COMBUSTION CHAMBER OF GAS TURBINE AND GAS TURBINE | 2019 |
|
RU2727946C1 |
| SLIDING COMPRESSOR ELEMENT, SLIDING ELEMENT BASE, SPIRAL ELEMENT AND COMPRESSOR | 2007 |
|
RU2387878C1 |
| TURBINE WITH SHEET METAL HOUSING WITH REINFORCING ELEMENT IN FORM OF CELLULAR STRUCTURE (VERSIONS) | 2015 |
|
RU2675295C2 |
| ROTARY COMPRESSOR | 2008 |
|
RU2470184C2 |
| MULTISTAGE TURBINE, PREFERABLY FOR ELECTRIC POWER STATIONS OPERATING ACCORDING TO ORGANIC RANKINE CYCLE | 2016 |
|
RU2716932C2 |
| TURBINE COMPRESSOR | 2001 |
|
RU2255271C2 |
| SCROLL COMPRESSOR | 2012 |
|
RU2564473C1 |
| COMPRESSOR AND OIL COOLING SYSTEM | 2010 |
|
RU2561807C2 |
